ONEWEB-0707, 61612
Orbit data source: Space-Track
ONEWEB-0707, 61612 is a payload satellite owned by Eut. One Web (UK) in LEO that was launched on Sun, 20 Oct 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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61612 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
UKRelated business
Manufacturer
One Web
Mission
Operational Commercial Communications
Bus & Motor
ARROW, Unknown motor
Mass
148 kg wet, ~140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 6.7 m
Radar Cross Section
3.464 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 ONEWEB-0707
1 61612U 24188U 25348.66275221 -.00000429 00000-0 -12662-2 0 9998
2 61612 87.8821 73.0330 0001044 99.8649 260.2597 13.10375153 59152Epoch: 2025-12-14T15:54Z
TLE epoch observation values (Epoch: 2025-12-14T15:54:21.790Z)
Latitude
0.00003°
Longitude
110.86976°
Altitude
1,224.73 km
Speed
7.242 km/s
True Right ascension
04h 52m 07s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
11:01:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,219.621 km
Perigee altitude
1,218.035 km
Semi-major axis
7,596.965 km
Eccentricity
0.0001
Inclination
87.8821°
RAAN
73.033°
Arg. of periapsis
99.8649°
True anomaly
260.24791°
Mean anomaly
260.2597°
Eccentric anomaly
260.2538°
Mean motion
3.2778 °/min
Orbital period
109.83 mins
BSTAR
-0.0012662
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Other satellites on launch #188 in the year 2024 (2024-10-20 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ONEWEB-0707 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-12-15 16:21:47.583Z | 38.588° NE | 2025-12-15 16:25:47.583Z | 74.742° E | 17.364° | 2025-12-15 16:29:47.583Z | 110.284° ESE |
| 12 mins | 2025-12-15 18:10:47.583Z | 355.305° N | 2025-12-15 18:16:47.583Z | 242.814° WSW | 44.127° | 2025-12-15 18:22:47.583Z | 188.397° SSW |
| 8 mins | 2025-12-16 04:42:47.583Z | 108.791° ESE | 2025-12-16 04:46:47.583Z | 69.871° E | 19.49° | 2025-12-16 04:50:47.583Z | 34.125° NE |
| 13 mins | 2025-12-16 06:29:47.583Z | 191.305° SSW | 2025-12-16 06:35:47.583Z | 283.08° WNW | 43.052° | 2025-12-16 06:42:47.583Z | 355.791° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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